View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 23432U 94083B 24357.85589519 .00000375 00000-0 14309-3 0 9994
2 23432 74.0326 315.8260 0006356 229.5715 150.9355 14.34149054569546
| Epoch (UTC): | 22 December 2024 20:32:29 |
| Eccentricity: | 0.0006356 |
| inclination: | 74.0326° |
| perigee height: | 773 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 315.8260° |
| argument of perigee: | 229.5715° |
| revolutions per day: | 14.34149054 |
| mean anomaly at epoch: | 150.9355° |
| orbit number at epoch: | 56954 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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